N2820W, cancelled Jul 20, 2010

Service difficulty reports · 57

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N2820W' AND deregistration_id = 'N2820W-2010-07-20'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR DL72W011512Panel · missingPANEL ON TOP OF RT WING TIP NAV LIGHT IS MISSING. REPLACED SAME.Sep 7, 2001 · N2820W · Boeing 727247 · Wing, Plate/SkinSDR DL72W011348Bear Strap · crackedTHE UPPER HINGE CUTOUT OF THE R1 DOOR OPENING WAS FOUND WITH A 2.5 INCH CRACK IN THE BEARSTRAP. THE SKIN WAS CUTOUT TO ACCESS THE BEARSTRAP AND THE CRACK IN THE BEARSTRAP STOP DRILLED. THE AREA WAS REPAIRED WITH TWO EXTERNAL ALUMINUM DOUBLERS PER ER/A 38Aug 17, 2001 · N2820W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W011133Battery · discharged1ST CLASS AISLE EMERGENCY LT INOP - REPLACED BATTERY PACKJul 8, 2001 · N2820W · Boeing 727247 · Emergency LightingSDR DL72W010225Indicator · inaccurateA/C DIVERSION DUE OUTBOARD FLAPS LOCKED OUT. INSPECTED T/E FLAPS. NO DEFECTS NOTED. OPERATED FLAPS. OP CK NML. SWAPPED INDICATORS AS PRECAUTION. FLAP IND AND OPN NML.Feb 8, 2001 · N2820W · Boeing 727247 · Trailing Flap Position Indicating SystemSDR DL72W010187Transmitter · failedOUTBOARD FLAPS WOULD NOT RETRACT. AIR TURNBACK. INSPECTED FLAP, NO DAMAGE NOTED. RETRACTED FLAPS, NORMAL OPERATED FLAPS AND NO DEFECTS NOTED. FOUND RT O/B FLAP TRANSMITTER CANNON PLUG EXCESSIVELY LOOSE. CLEANED AND RESECURED PLUG. REPLACED RT O/B TRANSMIFeb 1, 2001 · N2820W · Boeing 727247 · Trailing Edge Flap Control SystemSDR DL72W010024Skin · crackedA .375 INCH CRACK IN LOWER SKIN OF LT ELEVATOR I/B AND FWD OF TAB CONTROL ROD CUTOUT. REPAIRED PER SRM 55-20-3.Jan 5, 2001 · N2820W · Boeing 727247 · Elevator StructureSDR DL72W010003Clamp · stretchedAT 60 KTS ON T/O ROLL, LEFT STRUT PNEUMATIC DUCT PRESSURE WENT TO 6 O'CLOCK POSITION. ON CLIMBOUT, NR 1 ENG STRUT OVERHEAT LIGHT ILLUMINATED. NR 1 ENGINE THROTTLE BROUGHT TO IDLE. LIGHT EXTINGUISHED. FOUND WORN DUCT CLAMP ON ENG BLEED SUPPLY DUCT. REPLACED SAJan 1, 2001 · N2820W · Boeing 727247 · Pneumatic Distribution SystemSDR DL72W002316Battery · inoperativeLT FWD OVERWING EMERG LIGHTS INOP. CHNGD LT FWD OVERWING _EMERG LIGHT BATT PACK.Nov 28, 2000 · N2820W · Boeing 727247 · Emergency LightingSDR DL72W001483Line · leakingLOSS OF SYSTEM A FLUID IN FLIGHT WITH A PUMPS RUNNING WITH NO FLUID. FOUND LINE LEAKING AT LEFT MAIN GEAR DOOR ACTUATOR. REPLACED SAME. LEAK CKS GOOD. REPLACED EDP FILTERS PRECAUTIONARY. NO METAL FOUND IN FILTERS. ENGINE PUMPS CK GOOD. SERVICED HYD SYS Aug 4, 2000 · N2820W · Boeing 727247 · Hydraulic System, MainSDR DL72W001180Fuel Heater · intermittentNR 1 ENG FUEL HEAT VLV INTRANSIT LIGHT ILLUMINATED AFTER TAKEOFF. OIL TEMP IND HIGH. ACCOMPLISHED POM PROCEDURE. LIGHT REMAINED ON AND TEMP HIGH. WHEN FUEL DUMPING WAS STARTED THE LIGHT WENT OUT AND TEMP RETURNED TO NML. REPLACED NR 1 ENG FUEL HEAT VLV, OJun 19, 2000 · N2820W · Boeing 727247 · Fuel HeaterSDR DL72W001098Stiffener · crackedTPA LTR CHK C-1 06/05/00, I/B SPAR STIFFENER CRACKED AT NR 6 SLAT I/B TRACK. REPLACED PER MM 57-20-21Jun 5, 2000 · N2820W · Boeing 727247 · Leading Edge DevicesSDR DL72W000594Accessory Unit · malfunctionedAFTER EXPERIENCING MOD MOUNTAIN WAVE TURBULENCE AT FL330, GOT LEFT GEAR RED AND GREEN LIGHTS WITH GEAR HANDLE IN OFF OR UP POSITION. UPON GEAR DOWN SELECTION RED AND GREEN LIGHTS REMAINED ON. VISUALLY INSPECTED THE GEAR WERE DOWN. LANDED AND PINNED GEAR. Mar 29, 2000 · N2820W · Boeing 727247 · Landing Gear Position and WarningSDR DL72W992441Web · crackedREF SHIP 569 TPA LTR CHK B-2 11/04/99, .5 INCH CRACK AT LEFT TORQUE BOX VERT WEB LOWER LIGHTNING HOLE STA 1233. REPAIRED PER MM 53-11-0.Nov 4, 1999 · N2820W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W992440Web · crackedREF SHIP 569 TPA LTR CHK B-2 11-04-99, .5 INCH CRACK AT UPPER ROW OF RIVETS LT TORQUE BOX, VERT WEB STA 1305. REPAIRED PER MM 53-11-0.Nov 4, 1999 · N2820W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W992438Frame · crackedFOUND AT B-2 LETTER CK, AFT ENTRY DOOR LT CUTOUT FRAME CRACKED AT UPPER STOP FITTING STIFFENER. REPAIRED PER SRM 53-10-9.Nov 4, 1999 · N2820W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W991199Engine · failedNR 3 ENG POPPED AND SHUDDERED DURING APPLICATION OF T/O PWR, APPROX 1.6 EPR PRIOR TO INDICATION OF AIRSPEED. REPLACED ENGINE.May 29, 1999 · N2820W · Boeing 727247 · Engine (Turbine/Turboprop)SDR DL72W990825Skin · crackedWHILE ACCOMPLISHING HFEC INSPECTIONS PER SI 4-74176-12AD, REV F, CRACK INDICATIONS WERE NOTED BETWEEN BS 520 AND 681 AT S4R. ADDITIONALLY, GROUND DAMAGE WAS INDUCED TO THE AREA WHILE ACCOMPLISHING THE STANDARD REPAIR. REPAIRED PER ERA 332946-14AD, REV F.Apr 13, 1999 · N2820W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W990824Skin · crackedWHILE ACCOMPLISHING HFEC INSP PER SI 4-74176-12AD, REV F, A CRACK INDICATION WAS FOUND BETWEEN BS 681 AND BS 700; AT S4R. REPAIRED PER ERA 332945-14AD, REV A.Apr 13, 1999 · N2820W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W990694Rib · crackedUPPER CHORD ANGLE OF LT WING RIB AT WS 171.5 WAS FOUND WITH TWO CRACKS. THE CRACKS ARE LOCATED AT S16 AND S17. REPAIRED PER ERA 332958-14, REV A.Mar 30, 1999 · N2820W · Boeing 727247 · Wing, Rib/BulkheadSDR DL72W990693Frame · wornBS 1148 FRAME WAS FOUND WORN ON THE I/B HORIZ FLANGE RADIUS AT S22L. THE WEAR WAS CAUSED BY CONTACT WITH A HYD LINE. REPAIRED PER ERA 332949-14, REV A.Mar 30, 1999 · N2820W · Boeing 727247 · Fuselage Main, FrameSDR DL72W990691Skin · dentedA GOUGE WAS FOUND IN THE SKIN AT THE AFT EDGE OF THE C2 DOOR CUTOUT AT BS 990. THE DAMAGE IS LOCATED ABOVE S24R. THE SKIN, DOUBLER AND TRIPLER WERE DAMAGE, BUT NOT THE BEAR STRAP. REPAIRED PER ERA 332963-14, REV A.Mar 30, 1999 · N2820W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W990919Spar · crackedAFT SPAR CRACKED 22 FROM I/B END OF FLAP, THIS DAMAGED WAS REPAIRED PER MM 57-52-0 FIG 802 ON SHOP N/R 011630 LOCATED SHOP ORDER 709228.Mar 19, 1999 · N2820W · Boeing 727247 · Trailing Edge FlapsSDR DL72W990918Spar · damagedTEMP SPLICE AFT SPAR AT 57 AND 46 FROM I/B END OF FLAP. THIS DAMAGE WAS REPAIRED PER MM 57-52-0 FIG 802 ON SHOP N/R 011626, LISTED ON SHOP ORDER 709228.Mar 19, 1999 · N2820W · Boeing 727247 · Trailing Edge FlapsSDR DL72W990814Angle · crackedDURING SHOP INSPECTION, THE AFT LOWER CLOSEOUT SPAR ANGLE WAS FOUND CRACKED 2 PLACES 35 FROM IB END OF FLAP. A NEW SECTION OF SPAR ANGLE WAS DRILLED UP AND INSTALLED PER MM 57-52-01, FIG. 802.Mar 19, 1999 · N2820W · Boeing 727247 · Trailing Edge FlapsSDR DL72W990677Doubler · corrodedBONDED DOUBLER - CORRODED FS 72OB AND JUST BELOW STR 4R. REPAIRED PER SRM 53-30-4, METHOD 2, (H). WITHIN LIMITS PER SRM 53-30-4, METHOD 2 (H). OK TO T & P. TREATED PER SRM 53-30-4 METHOD 2 (J). PAINTED PER SRM 53-30-4 METHOD 2 STEP (K).Mar 19, 1999 · N2820W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W990769Stringer · crackedSTR RT CRACKED INSIDE VERT STA AT B/H STA 133.8 LOC INSIDE VERT STAB. BEGAN FABRICATING REPAIR ANGLE. FABRICATED REPAIR ANGLES PER M/M 55-30-0 PG 803. OK TO INSTALL REPAIR. INSTALLED REPAIR PER M/M 55-30-0 PG 803.Mar 18, 1999 · N2820W · Boeing 727247 · Vertical StabilizerSDR DL72W990684Doubler · corrodedBONDED DOUBLER, CORRODED FS 500 STR 3R TO 3L. REPAIRED PER SRM 53-30-4, METHOD 2 (H). WITHIN LIMITS PER SRM 53-30-4, METHOD 2 (H). OK TO T & P. TREATED PER SRM 53-30-4 METHOD 2 (J). PAINTED PER SRM 53-30-4 METHOD 2 STEP (K).Mar 18, 1999 · N2820W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W990683Doubler · corrodedBONDED DOUBLER, CORRODED FS 520 TO 540 FROM STR 4R TO 3L. REPAIRED PER SRM 53-30-4, METHOD 2 (H). WITHIN LIMITS PER SRM 53-30-4 METHOD 2, (H). OK TO T & P. TREATED PER SRM 53-30-4 METHOD 2 (J). PAINTED PER SRM 53-30-4 METHOD 2 STEP (K).Mar 18, 1999 · N2820W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W990682Doubler · corrodedDOUBLER CORRODED FS 560 TO 580 STR 1-2R. REPAIRED PER SRM 53-30-4, METHOD 2, H. WITHIN LIMITS PER SRM 53-30-4, METHOD 2 (H). OK TO T & P. TREATED PER SRM 53-30-4 METHOD 2 (J). PAINTED PER SRM 53-30-4 METHOD 2 STEP (K).Mar 18, 1999 · N2820W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W990681Doubler · corrodedBONDED DOUBLER, CORRODED FS 560 STR 4L TO 3L. REPAIRED PER SRM 53-30-4, METHOD 2 (H). WITHIN LIMITS PER SRM 53-30-4 METHOD 2, (H). OK TO T & P. TREATED PER SRM 53-30-4 METHOD 2 (J). PAINTED PER SRM 53-30-4 METHOD 2 STEP (K).Mar 18, 1999 · N2820W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W990680Doubler · corrodedBONDED DOUBLER, CORRODED FS 580 FROM STR 4L TO 4R. REPAIRED PER SRM 53-30-4, METHOD 2 (H). WITHIN LIMITS PER SRM 53-30-4 METHOD 2 (H). OK TO T & P. TREATED PER SRM 53-30-4 METHOD 2 (J). PAINTED PER SRM 53-30-4 METHOD 2 STEP (K).Mar 18, 1999 · N2820W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W990679Doubler · corrodedBONDED DOUBLERS, CORRODED FS 600 TO 620 AT STR 4R O/B SIDE OF STR AND SPLICE CORRODED ON I/B SIDE OF STR 22. REPAIRED PER SRM 53-30-4, METHOD 2, (H). WITHIN LIMITS PER SRM 53-30-4 METHOD 2, H. OK TO T & P. TREATED PER SRM 53-30-4 METHOD 2 (J). PAINTED PER Mar 18, 1999 · N2820W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W990678Doubler · corrodedBONDED DOUBLER, CORRODED FS 620 FROM STR 1R TO 4L. REPAIRED PER SRM 53-30-4, METHOD 2, (4). WITHIN LIMITS PER SRM 53-30-4, METHOD 2 (H). OK TO T & P. TREATED PER SRM 53-30-4 METHOD 2 (J). PAINTED PER SRM 53-30-4 METHOD 2 STEP (K).Mar 18, 1999 · N2820W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W990395Actuator · leakingLOST MAJORITY OF A SYS HYD FLUID WITH SYS A HYD PUMPS OFF. LEAK/LOSS STOPPED AT 1/2 GAL ON INDICATOR. FOUND NR 2 L/E FLAP ACTUATOR LEAKING. REPLACED ACTUATOR, LEAK CHKS NORMAL.Feb 25, 1999 · N2820W · Boeing 727247 · Leading Edge Slat ActuatorSDR DL72W990822Spar · crackedREAR SPAR CRACKED 19 AND 37 FROM I/B END. REPAIRED PER M/M 57-52-0.Jan 22, 1999 · N2820W · Boeing 727247 · Trailing Edge FlapsSDR DL72W990026Bulkhead Web · crackedTHE FS 1183 BULKHEAD WEB WAS FOUND WITH A CRACK AT WL 169 AND RBL 25. THE CRACK WAS REPAIRED WITH A DOUBLER ON A TIME LIMITED BASIS UNTIL THE FULL BAC S/B 727-53-0215 IS ACCOMPLISHED AT NEXT HMV. THE REPAIR WAS ACCOMPLISHED PER ER/A 366415-14.Jan 5, 1999 · N2820W · Boeing 727247 · Fuselage Main, BulkheadSDR DL72W982338Battery Pack · dischargedON S/C, FOUND RT OVERWING EMER LIGHT INOP. FOUND BATT PACK INOP. REPLACED SAME.Nov 13, 1998 · N2820W · Boeing 727247 · Emergency LightingSDR DL72W981411Actuator · leakingNR 2 SLAT ACTUATOR LEAKING, LOST HYDAULICS ON FINAL. REPLACED ACTUATOR.Jul 5, 1998 · N2820W · Boeing 727247 · Leading Edge Slat ActuatorSDR DL72W981353Battery Pack · dischargedOVERHEAD EMER LIGHT AT ROW 13 INOP. REPLACED BATT PACK, CK OK.Jun 27, 1998 · N2820W · Boeing 727247 · Emergency LightingSDR DL72W981191Web · crackedWEB CRACKED AT FASTENER STA 1239 RT SIDE AFT AIRSTAIR AREA REPAIR PER M/M 53-11-0.Jun 4, 1998 · N2820W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W981190Skin · separatedT/E RT ELEVATOR SEPARATING SEVERAL SMALL AREAS. REPAIR PER M/M 55-20-0.Jun 4, 1998 · N2820W · Boeing 727247 · Elevator, Plate/SkinSDR DL72W980387Battery Pack · dischargedON L/O, CHECK FOUND LT FIXED OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY PACK OF LT FIXED OVERWING EMERGENCY.Feb 14, 1998 · N2820W · Boeing 727247 · Emergency LightingSDR DL72W990022Skin · crackedFOUND ON A2 LETTER CK, .375 INCH CRACK LOWER I/B FASTENER HOLE AT THE L-4 WINDOW CUTOUT. REPAIRED PER SRM 53-30-3.Jan 5, 1998 · N2820W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W972585Hyd Line · crackedAT FLT LVL 290 HYD SYS-B QTY WENT TO ZERO. REPLACED HYD LINE AT B-FILTER MODULE.Dec 8, 1997 · N2820W · Boeing 727247 · Hydraulic System, MainSDR DL72W970599Cowl Flange · wornFLANGE/RING WORN AT 7 O'CLOCK POS FOR NR 2 ENGINE LT FWD COWL, LOC ON NR 2 LWR FIREWALL. REMOVED DAMAGE SECTION FRM 3 TO 9 O'CLOCK. INSTALLED REPAIR PER MM 53-11-0 PG 827.Mar 28, 1997 · N2820W · Boeing 727247 · Engine Cowling SystemSDR DL72W970588Web · crackedFOUND RT VERTICAL WEB CRACKED, FS 1303 ABOVE S-DUCT INSIDE VERTICAL FIN SAME COND LWR LT SIDE OF WEB. REPAIRED BOTH SIDES PER SRM 53-10-04, FIG 17.Mar 26, 1997 · N2820W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W970587Stringer · crackedFOUND VERTICAL FIN LT SIDE, 3RD STR FROM REAR SPAR CRACKED 3RD BAY, ABOVE FIN ACCESS PNL 9504. REPAIRED PER M/M 55-33-00, FIG 803.Mar 26, 1997 · N2820W · Boeing 727247 · Vertical StabilizerSDR DL72W970048Battery · dischargedFWD EMERGENCY FLASHLIGHT WON,T BLINK. REPLACED FLASHLIGHT BATTERY AND BULB, OPERATIONAL TEST NML.Jan 10, 1997 · N2820W · Boeing 727247 · Emergency LightingSDR DL72W961565Generator · failedNR 1 GEN ALREADY ON MCO NR 2 GEN FAILED. NR 2 ENGINE CSD/ GEN CHANGE IN PROGRESS.Jul 1, 1996 · N2820W · Boeing 727247 · AC Generator-AlternatorSDR DL72W961316Rib · crackedRIB NR 21 CRACKED. REPAIRED PER MM 57-54-0.May 29, 1996 · N2820W · Boeing 727247 · Leading Edge Devices
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